FR2833197B1 - METHOD FOR MANUFACTURING A BLADE RING - Google Patents

METHOD FOR MANUFACTURING A BLADE RING

Info

Publication number
FR2833197B1
FR2833197B1 FR0115757A FR0115757A FR2833197B1 FR 2833197 B1 FR2833197 B1 FR 2833197B1 FR 0115757 A FR0115757 A FR 0115757A FR 0115757 A FR0115757 A FR 0115757A FR 2833197 B1 FR2833197 B1 FR 2833197B1
Authority
FR
France
Prior art keywords
manufacturing
blade ring
blade
ring
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
FR0115757A
Other languages
French (fr)
Other versions
FR2833197A1 (en
Inventor
Gerard Michel Roland Gueldry
Jacky Naudet
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA Moteurs SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SNECMA Moteurs SA filed Critical SNECMA Moteurs SA
Priority to FR0115757A priority Critical patent/FR2833197B1/en
Priority to US10/492,542 priority patent/US20040244195A1/en
Priority to PCT/FR2002/004201 priority patent/WO2003055634A1/en
Priority to JP2003556201A priority patent/JP2005513343A/en
Priority to EP02293013A priority patent/EP1317987A1/en
Publication of FR2833197A1 publication Critical patent/FR2833197A1/en
Application granted granted Critical
Publication of FR2833197B1 publication Critical patent/FR2833197B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • F01D9/044—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators permanently, e.g. by welding, brazing, casting or the like
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K10/00—Welding or cutting by means of a plasma
    • B23K10/02—Plasma welding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/006—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine wheels
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR0115757A 2001-12-06 2001-12-06 METHOD FOR MANUFACTURING A BLADE RING Expired - Fee Related FR2833197B1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR0115757A FR2833197B1 (en) 2001-12-06 2001-12-06 METHOD FOR MANUFACTURING A BLADE RING
US10/492,542 US20040244195A1 (en) 2001-12-06 2002-12-06 Method for making a blade ring
PCT/FR2002/004201 WO2003055634A1 (en) 2001-12-06 2002-12-06 Method for making a blade ring
JP2003556201A JP2005513343A (en) 2001-12-06 2002-12-06 Manufacturing method of blade ring
EP02293013A EP1317987A1 (en) 2001-12-06 2002-12-06 Manufacturing process of a turbine rotor ring

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0115757A FR2833197B1 (en) 2001-12-06 2001-12-06 METHOD FOR MANUFACTURING A BLADE RING

Publications (2)

Publication Number Publication Date
FR2833197A1 FR2833197A1 (en) 2003-06-13
FR2833197B1 true FR2833197B1 (en) 2004-02-27

Family

ID=8870161

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0115757A Expired - Fee Related FR2833197B1 (en) 2001-12-06 2001-12-06 METHOD FOR MANUFACTURING A BLADE RING

Country Status (5)

Country Link
US (1) US20040244195A1 (en)
EP (1) EP1317987A1 (en)
JP (1) JP2005513343A (en)
FR (1) FR2833197B1 (en)
WO (1) WO2003055634A1 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2871847B1 (en) * 2004-06-17 2006-09-29 Snecma Moteurs Sa MOUNTING A TURBINE DISPENSER ON A COMBUSTION CHAMBER WITH CMC WALLS IN A GAS TURBINE
EP2264284B1 (en) * 2009-06-18 2015-01-28 Techspace Aero S.A. Method for manufacturing vanes built into a shroud ring and stator ring obtained according to the method
US10471212B2 (en) 2009-10-29 2019-11-12 W. L. Gore & Associates, Inc. Silicone free drug delivery devices
US8777583B2 (en) * 2010-12-27 2014-07-15 General Electric Company Turbine airfoil components containing ceramic-based materials and processes therefor
CN106141597B (en) * 2016-08-31 2018-08-10 宜昌船舶柴油机有限公司 Gas turbine exhaust thermal insulation layer front processing tool and processing method
CN109968084B (en) * 2019-04-04 2020-07-17 哈尔滨汽轮机厂有限责任公司 Clamping device for turning inner hole of guide vane of gas turbine
CN110539132B (en) * 2019-08-19 2020-12-22 西北工业大学 Manufacturing method of blisk with precise forming of additive manufacturing and electrolytic machining
US11879360B2 (en) 2020-10-30 2024-01-23 General Electric Company Fabricated CMC nozzle assemblies for gas turbine engines
CN114799754B (en) * 2022-04-28 2023-02-24 苏州千机智能软件有限公司 Stator blade ring machining method, electronic equipment and machining equipment

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2109821B (en) * 1981-08-05 1985-08-14 Lucas Ind Plc Method of manufacturing bearing blocks
SE446606B (en) * 1981-08-27 1986-09-29 Stal Laval Turbin Ab VIEW TO MANUFACTURE SHOOTING RINGS AND SHEETS WITH SHOVERS FOR ROTATING MACHINES LIKE COMPRESSORS OR TURBINES
US4573876A (en) * 1983-02-14 1986-03-04 Williams International Corporation Integral bladed disk
CH670406A5 (en) * 1987-03-19 1989-06-15 Bbc Brown Boveri & Cie
US5273708A (en) * 1992-06-23 1993-12-28 Howmet Corporation Method of making a dual alloy article
US5553370A (en) * 1995-02-09 1996-09-10 Pepe; John Method for repair of steam turbine blades
US6049978A (en) * 1996-12-23 2000-04-18 Recast Airfoil Group Methods for repairing and reclassifying gas turbine engine airfoil parts
DE19712868C1 (en) * 1997-03-27 1998-10-01 Mtu Muenchen Gmbh Tip repair method for gas turbine blades
US6305459B1 (en) * 1999-08-09 2001-10-23 Ford Global Technologies, Inc. Method of making spray-formed articles using a polymeric mandrel

Also Published As

Publication number Publication date
WO2003055634A1 (en) 2003-07-10
FR2833197A1 (en) 2003-06-13
US20040244195A1 (en) 2004-12-09
EP1317987A1 (en) 2003-06-11
JP2005513343A (en) 2005-05-12

Similar Documents

Publication Publication Date Title
FR2825834B1 (en) METHOD FOR MANUFACTURING A SEMICONDUCTOR DISSIVE
FR2831331B1 (en) METHOD FOR MANUFACTURING A MICRO-BATTERY
FR2836486B1 (en) PROCESS FOR PRODUCING A METALLIC ELEMENT
FR2833838B1 (en) METHOD FOR MANUFACTURING A TABLET INCLUDING A MORPHINIC ANALGESIC AND TABLET OBTAINED
FR2871398B1 (en) METHOD FOR MANUFACTURING A TURBINE STATOR CASTER
FR2855439B1 (en) METHOD FOR MANUFACTURING A HOLLOW DAWN FOR TURBOMACHINE
FR2858714B1 (en) METHOD FOR MANUFACTURING A SEMICONDUCTOR DEVICE
FR2867095B1 (en) METHOD FOR MANUFACTURING A HOLLOW DAWN FOR TURBOMACHINE
FR2788386B1 (en) METHOD FOR MANUFACTURING A MICRO-ACTUATOR USING PHOTOLITHOGRAPHY
FR2833197B1 (en) METHOD FOR MANUFACTURING A BLADE RING
FR2864330B1 (en) METHOD FOR MANUFACTURING A MULTIPOLAR MAGNETIC ENCODER
ITMI20020092A1 (en) A PLANT
FR2819635B1 (en) METHOD FOR MANUFACTURING INTERCONNECTION NETWORKS
FR2860445B1 (en) METHOD FOR MANUFACTURING A MOLD AND MOLD OBTAINED
FR2855440B1 (en) METHOD FOR MANUFACTURING A HOLLOW DAWN FOR TURBOMACHINE
FR2842137B1 (en) METHOD FOR MANUFACTURING A BELOW BELLOW
FR2837216B1 (en) METHOD FOR MANUFACTURING A MOLDED ELEMENT
FR2861719B1 (en) METHOD FOR MANUFACTURING A PREFORM
FR2825376B1 (en) METHOD FOR MANUFACTURING AN ALLOY WEAR-RESISTANT MOLDED ARTICLE A1-Si
FR2827294B1 (en) DISCONTINUOUS PROCESS FOR THE MANUFACTURE OF A POLYAMIDE
DK1379128T3 (en) A plant
FR2825535B1 (en) METHOD OF MANUFACTURING A ROTOR
FR2832351B1 (en) PROCESS FOR MANUFACTURING A SEAL
FR2822817B1 (en) METHOD FOR MANUFACTURING MICRO-FACTORY MEMBRANE STRUCTURE
FR2819437B1 (en) PROCESS FOR MANUFACTURING A CRANKSHAFT

Legal Events

Date Code Title Description
CD Change of name or company name
ST Notification of lapse

Effective date: 20060831